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Spacecraft Valves - Mars Science Laboratory (MSL)

12 Spacecraft Valves from 1 Manufacturer meet your specification.
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  • Mission: Mars Science Laboratory (MSL)
Torque Motor Latch Valve (TMLV) Image
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4000 psi Space Qualified Latching Valve

Spacecraft Valve from Moog
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SKU:Torque Motor Latch Valve (TMLV)
Space Heritage:
Yes
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
1.13 kg
Valve Type:
Torque Motor Latch Valve
Operating Pressure:
276 bar
Proof Pressure:
414 bar
Response Time:
50 ms
External Leakage Time:
1.0 x 10-6 scc/s
Internal Leakage Time:
1 x 10-3 scc/s
Life Cycle:
1000 Cycles
Storage Temperature:
-40 to 79 Degree C
Operating Temperature:
-29 to 68 Degree C
Dimension:
7.298 x 2.54 x 3.899 Inches
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Thrust Single Seat

Spacecraft Valve from Moog
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SKU:051-271
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
30 g
Valve Type:
Monopropellant Thruster Valve
Supply Voltage:
24 to 32 V
Power Consumption:
10.4 W
Operating Pressure:
26.6 bar
Proof Pressure:
61.1 bar
Response Time:
1 ms
External Leakage Time:
1.0 x 10-6 scc/s
Internal Leakage Time:
0.4 scc/hr
Life Cycle:
1000000 Cycles
Operating Temperature:
4.4 to 149 Degree C
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Thust Redundant Seat

Spacecraft Valve from Moog
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SKU:051-346D
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
218 g
Valve Type:
Monopropellant Thruster Valve
Supply Voltage:
24 to 37 V
Power Consumption:
8.69 W
Operating Pressure:
27.6 bar
Proof Pressure:
103.4 bar
Response Time:
10 ms
External Leakage Time:
1.0 x 10-6 scc/s
Internal Leakage Time:
0.4 scc/hr
Life Cycle:
1000000 Cycles
Operating Temperature:
4.4 to 149 Degree C
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Thrust Single Seat

Spacecraft Valve from Moog
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SKU:51-288
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
230 g
Valve Type:
Monopropellant Thruster Valve
Supply Voltage:
22 to 32 V
Power Consumption:
26.5 W
Operating Pressure:
34.5 bar
Proof Pressure:
103 bar
Response Time:
15 ms
External Leakage Time:
1.0 x 10-6 scc/s
Internal Leakage Time:
0.2 scc/hr
Life Cycle:
100000 Cycles
Operating Temperature:
4.4 to 149 Degree C
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Thrust Single Seat

Spacecraft Valve from Moog
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SKU:53-291B
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
1134 g
Valve Type:
Monopropellant Thruster Valve
Supply Voltage:
98 to 136 V
Power Consumption:
122 W
Operating Pressure:
19 bar
Proof Pressure:
31 bar
Response Time:
20 to 30 ms
External Leakage Time:
1.0 x 10-6 scc/s
Internal Leakage Time:
3.6 scc/hr
Life Cycle:
100000 Cycles
Operating Temperature:
4.4 to 149 Degree C
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Thust Redundant Seat

Spacecraft Valve from Moog
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SKU:051-178-5
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
182 g
Valve Type:
Bipropellant Thruster Valve
Supply Voltage:
49 to 51 V
Power Consumption:
217 W
Operating Pressure:
19 bar
Proof Pressure:
52.8 bar
Response Time:
6 ms
External Leakage Time:
1.0 x 10-6 scc/s
Internal Leakage Time:
3 scc/hr
Life Cycle:
1000000 Cycles
Operating Temperature:
4.4 to 121 Degree C
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Thrust Single Seat

Spacecraft Valve from Moog
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SKU:53-247A
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
545 g
Valve Type:
Bipropellant Thruster Valve
Supply Voltage:
23.5 to 31.1 V
Power Consumption:
42 W
Operating Pressure:
25 bar
Proof Pressure:
70 bar
Response Time:
15 to 22 ms
External Leakage Time:
1.0 x 10-5 scc/s
Internal Leakage Time:
5 scc/hr
Life Cycle:
100000 Cycles
Operating Temperature:
0 to 50 Degree C
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Thrust Single Seat

Spacecraft Valve from Moog
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SKU:53-200C
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
409 g
Valve Type:
Bipropellant Thruster Valve
Supply Voltage:
20 to 32 V
Power Consumption:
47.6 W
Operating Pressure:
19 bar
Proof Pressure:
31 bar
Response Time:
20 to 30 ms
External Leakage Time:
1.0 x 10-4 scc/s
Internal Leakage Time:
5 scc/hr
Life Cycle:
5000 Cycles
Operating Temperature:
4.4 to 93.3 Degree C
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Low Pressure Stainless Steel with Cover

Spacecraft Valve from Moog
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SKU:050E880
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
209 g
Valve Type:
Fill & Drain Service Valve
Operating Pressure:
43.8 bar
Proof Pressure:
66.2 bar
External Leakage Time:
1.0 x 10-6 scc/s
Internal Leakage Time:
1.0 x 10-6 scc/s
Life Cycle:
150 Cycles
Operating Temperature:
-7.2 to 60 Degree C
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Low Pressure Titanium with Cover

Spacecraft Valve from Moog
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SKU:050E835
Mission:
Mars Science Laboratory (MSL), AEHF, TacSat-2, ISS & Resupply (Columbus, MPLM, and ATV), QinetiQ Comsat, BepiColombo
Mass:
209 g
Valve Type:
Fill & Drain Service Valve
Operating Pressure:
43.8 bar
Proof Pressure:
66.2 bar
External Leakage Time:
1.0 x 10-6 scc/s
Internal Leakage Time:
1.0 x 10-6 scc/s
Life Cycle:
150 Cycles
Operating Temperature:
-7.2 to 60 Degree C
more info
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